Model of structure of re-entry vehicle mounted on multistage rocket booster is constructed; dynamic environment to which it is subjected during ballistic flight is considered as to source and character of forces involved; dynamic model of system is presented and equations of motion written; dynamic model of re-entry vehicle-shaker combination is presented; results show that simulation of shear and slope at interface of vehicle during vibration test by proper fixture design is feasible using methods and approximations included in report.


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    Titel :

    Simulation of in-flight lateral bending modes for electrodynamic shaker testing


    Weitere Titelangaben:

    AIAA -- Tech Paper


    Beteiligte:
    Gross, D.V. (Autor:in) / Kachadourian, G. (Autor:in)

    Kongress:

    Meeting of the AIAA -- Simulation for Aerospace Flight Conference ; 1963 Re-entry



    Erscheinungsdatum :

    1963


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    SHOCK TESTING WITH THE ELECTRODYNAMIC SHAKER

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